prueba A320

1.- Both autopilots can be engaged and active in any phase of flight. A.- True. B.- False.

2.- If the SPD/MACH knob on the FCU is not pulled within a predetermined time to engage selected speed: A.- The selection can be made at any time. B.- The selection is lost and dashes are re-displayed. C.- The selection is lost and the disply goes blank.

3.- When the altitude knob on the FCU is pulled: A.- The altitude is armed. B.- The current altitude is canceled. C.- Open Climb or descent engages.

4.- You can disengage the EXPEDITE mode by: A.- Pressing the EXPED switch on the FCU. B.- Engaging another vertical mode. C.- Either A or B.

5.- Can the autopilot be used for a single engine approach and auto land?. A.- Yes. B.- No.

6.- What happens if you push the V/S knob?. A.- Engage the V/S mode. B.- Command a zero vertical rate (ALT HOLD). C.- Reverts to Managed Climb.

7.- APPR pb. is used to arm/engage the guidance modes related to the approach: A.- Selected on the navigation radios. B.- Inserted into the flight plan (ILS only). C.- Inserted into the flight plan (ILS or non ILS).

8.- For autoland, both A/Ps must be connected. A.- True. B.- False.

9.- What happens if you press the EXPED pb?. A.- Speed is set to 340 knots for climb and green dot for descent. B.- Speed is set to green dot for climb and 340 knits for descent. C.- Decelerated speed aprroach is selected.

10.- When can you select both A/Ps at the same time?. A.- After you select both navigation radios on al ILS frequency. B.- Only after the approach mode is armed and an ILS app is interesed into the flight plan. C.- Never.

1.- Which of the following will automatically reset after landing?. A.- THS. B.- Rudder trim. C.- Both are correct.

2.- The spoiler panels are the only flight control surfaces with no redundant control. A.- True. B.- False.

3.- Which of the following statements is correct concerning the elevator aileron computers (ELAC's)?. A.- Three computers which achieve normal elevator, stabilizer, and aileron control. B.- Two computers which achieve normal elevator and aileron control. C.- Two computers which achieve normal and standby control of the elevators, ailerons, ands THS.

4.- When the landing gear is extended, pitch alternate law: A.- Remains the same. B.- Degrades to pitch direct law. C.- Degrades to pitch backup law.

5.- Is there any rudder pedal feedback for the yaw damping and turn coordination functions?. A.- Yes. B.- No.

6.- What are the rudder trim rates?. A.- A/P on - 5 deg/sec, A/P off - 1 deg/sec. B.- A/P on - 2 1/5 deg/sec, A/P off - 5 deg/sec. C.- A/P on - 3 deg/sec, A/P off - 6 deg/sec. D.- A/P on - 5 deg/sec, A/P off - 6 deg/sec.

7.- The wing tip brakes, once activated: A.- Lock both the slats and flaps in their current position. B.- Lock only the flaps in their current position. C.- Lock only the slats in their current position. D.- Lock only the affected high lift system surfaces with in their current position.

8.- In Normal Law, what are the limits of Pitch Attitude protections with flaps Full. A.- 30° nose up. B.- 35° nose up progressively reduced to 20°. C.- 25° nose up, progressively reduced to 20° at low speed. D.- There is no limit.

9.- The FAC's primarily control which control surface?. A.- Elevator. B.- Rudder. C.- Aileron. D.- Elevator and aileron.

10.- What happens to the rudder limits if both FAC's fault?. A.- The limit freezes at the fault condition until Flaps 1 is selected. B.- The limit freezes at the fault condition until Flaps 5 is selected. C.- The limit freezes at the fault condition until Flaps 1 is selected. Then resets to the low speed limits for increased control.

11.- With the aircraft in Pitch Alternate Law, roll is in _______ Law. A.- Direct. B.- Normal. C.- Alternate.

12.- What condition will cause auto flap retraction?. A.- Exceed 210 kts at Flaps 1. B.- Exceed 190 kt at Flaps 1. C.- Exceed 195 kt at Flaps 1. D.- Exceed 190 kt with Flaps 1 white extending the speedbrake lever.

13.- The FLAP lever sends signal to Slat Flap Control Computer (SFCC) to command movement. A.- True. B.- False.

14.- Selection of flaps 1 in flight will select which of the following configurations?. A.- Slats 1 and flaps 1 (1+F). B.- Slats 0 and flaps 1 (0+F). C.- Slats 1 and flaps 0 (1). D.- Slats 1 and flaps 5 (1+F).

15.- Which of the following controls and monitors flaps and slats?. A.- Two ELAC's. B.- Wing tip brakes. C.- One slat flap control computer (SFCC). D.- Two slat flap control computer (SFCC's).

16.- Can you manually trim the rudder with the autopilot engaged?. A.- Yes. B.- No.

17.- The Ground Mode is different in Alternative Law. A.- True. B.- False.

18.- What control surfaces do the FACs control?. A.- The elevators. B.- The spoilers. C.- The rudder. D.- All the above.

19.- If angle of attack protection is active or flaps are in the configuration Full: A.- Speed brake extension is inhibited. B.- Aileron travel is reduced. C.- Speed brake extension travel is reduced.

20.- Automatic pitch trim is inhibited when: A.- Radio altitude is below 50 feet (100 feet with autopilot coupled). B.- Bank angle is greater than 33 degrees. C.- Load factor is less than 1G. D.- Both A and B.

21.- In pich normal law, the elevator control changes from the normal mode to a protection mode when the angle of attack is greater than: A.- Alpha Max. B.- Alpha Prot. C.- Alpha Floor.

22.- Roll control in NORMAL LAW is achieved with: A.- Ailerons and spoilers. B.- Ailerons, spoilers, and rudder. C.- Ailerons, spoilers 2-5, and rudder.

23.- When ground spoilers deploy automatically: A.- All ten-spoiler panels fully deploy. B.- Four spoiler panels on each wing deploy. C.- All ten-spoiler panels deploy half way. D.- Six spoiler panels on each wing deploy.

24.- Selection of flaps 1 in flight will select which of the following configurations?. A.- Slats 1 and flaps 1 (1+F). B.- Slats 0 and flaps 1 (0+F). C.- Slats 1 and flaps 0 (1). D.- Slats 1 and flaps 5 (1+F).

25.- When the landing gear is extended, pitch alternate law: A.- Remains the same. B.- Degrades to pitch direct law. C.- Degrades to pitch backup law.

26.- The A-320 flight control sufaces are _______ controlled and _______ actuated. A.- Electrically, hydraulically. B.- Mechanically, hydraulically. C.- Electrically, electrically.

27.- Sidesticks provide electrical signals to the flight control computers, if both sidesticks are operated: A.- The inputs cancel each other. B.- Both inputs are algebraically added. C.- The F/O input is overridden by the CAP input.

28.- Roll control is achieved by: A.- Ailerons. B.- Ailerons and rudder. C.- One aileron and four spoilers on each wing.

29.- When the flaps are extended, the ailerons: A.- Go to the centering mode. B.- Pich up 5 degrees. C.- Droop 5 degrees.

30.- If electrical power to a SEC fails: A.- The affected spoilers automatically retracts. B.- All spoilers automatically retract. C.- The affected spoilers remains in the last commanded position.